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Aircraft Design
1673-4599
2002 Issue 1
FATIGUE LIFE ANALYSIS OF THE LEADING-EDGE FLAP ON X MODEL AIRCRAFT
li yong gang ; li gang ; li ze jin
..............page:1-4
ANTI-GUST CONTROL METHOD FOR DEAD RECKONING OF UAV
cao yun feng ; tao yong ; su bing wei ; shen yong zuo
..............page:5-8
DESIGN-ORIENTED FINITE ELEMENT AUTO-MODELING TO AIRCRAFT WING STRUCTURES
deng yang chen ; liao jia ju ; zhang zuo ning ; chen wen pu ; sun xian xue ; wang qing tai ; zuo zheng neng
..............page:9-13
STUDYING ON FAULT DATABASE MODEL OF AIRCRAFT LANDING GEAR AND REALIZATION
song yun xue ; shi yong sheng ; qian li bin
..............page:14-17
THE ANALYSIS AND DESIGN OF THE ADHESIVE BONDING REPAIR OF THE DAMAGED COMPOSITE COMPONENTS
meng fan zuo ; chen shao jie ; dong shan yan ; tong xiao yan
..............page:18-21
RELIABILITY CONTROL FOR ELECTRONIC PART IN ENGINEERING DEVELOPMENT
shi peng ; ma hai feng
..............page:22-25
AN INVESTIGATION ON INSTALLATION OF HEAD-UP DISPLAY ON AIRCRAFT
li chun liang ; li zuo
..............page:34-38
THE FIRE PROTECTION OF PERMANENT MAGNET AERO-GENERATOR
kang xiao rong ; zhu yao zhong ; hu ze yan
..............page:39-42
EMC DESIGN FOR COMPUTER SYSTEM
wang tian shun
..............page:43-48
THE MEASUREMENT OF ROTATIONAL INERTIA FOR SMALL MISSILES
li hong ru ; yu zhi hui
..............page:61-67
TEST QUALITY MANAGEMENT
dai wei qun ; yao wen zeng
..............page:73-76